CA2462517A1 - Carrying or guiding device for aircraft components - Google Patents
Carrying or guiding device for aircraft components Download PDFInfo
- Publication number
- CA2462517A1 CA2462517A1 CA002462517A CA2462517A CA2462517A1 CA 2462517 A1 CA2462517 A1 CA 2462517A1 CA 002462517 A CA002462517 A CA 002462517A CA 2462517 A CA2462517 A CA 2462517A CA 2462517 A1 CA2462517 A1 CA 2462517A1
- Authority
- CA
- Canada
- Prior art keywords
- carrier
- carrying
- joints
- guiding device
- aircraft components
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The invention relates to a carrying or guiding device (1) for aircraft components, especially for a landing flap which is arranged on an aircraft wing. The inventive device comprises a carrier (2) having an essentially U- shaped profile and essentially parallel lateral walls (3, 4). In order to produce one such device in such a way that it weighs as little as possible, has the required mechanical properties, and is as easy to produce and to assemble as possible, the carrier (2), and preferably one covering plate (20 ) arranged on the open side of the carrier (2), are produced from fibre reinforced plastic, especially carbon fibre reinforced plastic (CFRP). The connection between the carrier (2) and the covering plate (20) and possible connection elements (21) is preferably carried out by means of glued joints and, if necessary, additional riveted joints or screwed joints.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT0169001A AT410656B (en) | 2001-10-24 | 2001-10-24 | TRAG- OR GUIDE DEVICE FOR AIRCRAFT COMPONENTS |
ATA1690/2001 | 2001-10-24 | ||
PCT/AT2002/000266 WO2003035469A1 (en) | 2001-10-24 | 2002-09-16 | Carrying or guiding device for aircraft components |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2462517A1 true CA2462517A1 (en) | 2003-05-01 |
CA2462517C CA2462517C (en) | 2008-11-18 |
Family
ID=3688670
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002462517A Expired - Fee Related CA2462517C (en) | 2001-10-24 | 2002-09-16 | Carrying or guiding device for aircraft components |
Country Status (7)
Country | Link |
---|---|
US (1) | US7011276B2 (en) |
EP (1) | EP1438230B1 (en) |
AT (1) | AT410656B (en) |
CA (1) | CA2462517C (en) |
DE (1) | DE50202945D1 (en) |
ES (1) | ES2240805T3 (en) |
WO (1) | WO2003035469A1 (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004006940B4 (en) | 2004-02-12 | 2009-02-26 | Airbus Deutschland Gmbh | Landing flap guide for aircraft |
DE102005017307A1 (en) * | 2005-04-14 | 2006-10-26 | Airbus Deutschland Gmbh | Landing flap drive system for use in aircraft, is connected to track of landing flap which is operated by drive motor |
US7249735B2 (en) * | 2005-06-30 | 2007-07-31 | The Boeing Company | Translating conduit apparatus for an airplane or equipment |
DE102007048449A1 (en) * | 2007-10-10 | 2009-04-23 | Eads Deutschland Gmbh | Lift flaps support system |
DE102008028542B4 (en) * | 2008-06-16 | 2012-07-12 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Method and apparatus for depositing a layer on a substrate by means of a plasma-enhanced chemical reaction |
DE102008047793B4 (en) | 2008-09-17 | 2017-03-30 | Airbus Defence and Space GmbH | Load introduction element |
JP5562575B2 (en) * | 2009-04-27 | 2014-07-30 | ナブテスコ株式会社 | Aircraft actuator |
JP2011116147A (en) * | 2009-11-30 | 2011-06-16 | Nabtesco Corp | Reaction link |
JP5552340B2 (en) * | 2010-03-15 | 2014-07-16 | ナブテスコ株式会社 | Actuator and link manufacturing method, actuator and link design method, actuator and link |
GB201111922D0 (en) | 2011-07-12 | 2011-08-24 | Airbus Operations Ltd | Leading edge rib assembly |
FR2990187B1 (en) * | 2012-05-07 | 2015-01-30 | Airbus Operations Sas | BEAM IN COMPOSITE MATERIAL INCORPORATING A CLOSED SECTION REINFORCEMENT |
DE102014106930A1 (en) * | 2014-05-16 | 2015-11-19 | Airbus Operations Gmbh | Load-bearing cladding element for a flap adjustment mechanism and aircraft with such a cladding element |
EP3025955B1 (en) * | 2014-11-26 | 2019-06-19 | Airbus Defence and Space GmbH | High lift system |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2112154A (en) * | 1935-08-02 | 1938-03-22 | Randolph F Hall | Airplane |
US4471928A (en) * | 1980-08-13 | 1984-09-18 | The Boeing Company | Extendible airfoil track assembly |
US4451528A (en) * | 1981-03-30 | 1984-05-29 | Ni Industries, Inc. | Composite fiber reinforced member and method |
US4542869A (en) * | 1983-06-23 | 1985-09-24 | Mcdonnell Douglas Corporation | Flap mechanism |
GB8718977D0 (en) * | 1987-08-11 | 1987-09-16 | British Aerospace | Trailing edge flaps |
US5171510A (en) * | 1988-06-08 | 1992-12-15 | Aerospatiale Societe Nationale Industrielle | Method of producing a frame made of a composite material, especially for the fuselage of an aircraft |
GB8819535D0 (en) * | 1988-08-17 | 1988-09-21 | British Aerospace | Wing flap track beams for aircraft |
GB9024387D0 (en) * | 1990-11-09 | 1991-01-02 | British Aerospace | Carbon fibre composite wing manufacture |
DE4107556C1 (en) * | 1991-03-08 | 1992-05-14 | Deutsche Airbus Gmbh, 2000 Hamburg, De | |
FR2679866B1 (en) * | 1991-08-02 | 1993-11-05 | Piquereau Jean Yves | SMALL SIZE CARGO AIRCRAFT. |
SE502781C2 (en) * | 1993-08-20 | 1996-01-15 | Transman Ab | Universal beam for moving load |
JP3839080B2 (en) * | 1995-06-21 | 2006-11-01 | 富士重工業株式会社 | Structure of fiber-reinforced composite material and manufacturing method thereof |
US5788190A (en) * | 1996-10-22 | 1998-08-04 | The Boeing Company | Slotted cruise trailing edge flap |
US6237304B1 (en) * | 1997-07-18 | 2001-05-29 | Henkel Corporation | Laminate structural bulkhead |
US6739553B2 (en) * | 2000-04-05 | 2004-05-25 | Bell Helicopter Textrom, Inc. | K-spar configuration for bonded wing construction |
US6719870B2 (en) * | 2000-12-15 | 2004-04-13 | The Boeing Company | Fastenerless internal support for hollow structures |
JP4574086B2 (en) * | 2001-09-03 | 2010-11-04 | 富士重工業株式会社 | Method for manufacturing composite wing and composite wing |
-
2001
- 2001-10-24 AT AT0169001A patent/AT410656B/en not_active IP Right Cessation
-
2002
- 2002-09-16 WO PCT/AT2002/000266 patent/WO2003035469A1/en not_active Application Discontinuation
- 2002-09-16 DE DE50202945T patent/DE50202945D1/en not_active Expired - Lifetime
- 2002-09-16 ES ES02774139T patent/ES2240805T3/en not_active Expired - Lifetime
- 2002-09-16 US US10/493,604 patent/US7011276B2/en not_active Expired - Lifetime
- 2002-09-16 CA CA002462517A patent/CA2462517C/en not_active Expired - Fee Related
- 2002-09-16 EP EP02774139A patent/EP1438230B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
WO2003035469A1 (en) | 2003-05-01 |
AT410656B (en) | 2003-06-25 |
US7011276B2 (en) | 2006-03-14 |
CA2462517C (en) | 2008-11-18 |
DE50202945D1 (en) | 2005-06-02 |
ATA16902001A (en) | 2002-11-15 |
ES2240805T3 (en) | 2005-10-16 |
EP1438230A1 (en) | 2004-07-21 |
US20050082434A1 (en) | 2005-04-21 |
EP1438230B1 (en) | 2005-04-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20200916 |